SUBMERGED PLANING SURFACE THAT PROVIDES HYDRODYNAMIC LIFT IN A LIQUID AT HIGH SPEED

Abstract

One embodiment of submerged blades (101) that provide hydrodynamic force to a vessel or aircraft (117) that can lift it above the surface of the water (106) at high speed by creating thrust with a single wetted high pressure surface (111), the low pressure surface (112) being covered with a gas filled void in the liquid, thus preventing sudden loss of lift as speed increases due to cavitation or surface venting. Other embodiments are described and shown.

Description

CROSS-REFERENCED TO RELATED APPLICATION

This application claims the benefit of PPA Ser. No. 61/977,024, filed 2014 Apr. 8, PPA Ser. No. 62/049,867 filed 2014 Sep. 12 with the USPTO and PCT/US2015/024215 filed 2015 Apr. 3 by the present inventor.

FEDERALLY SPONSORED RESEARCH

None.

BACKGROUND

This invention relates to articles such as hydrofoils and other submerged lifting or thrusting articles such as, rudders, propeller blades, turbine blades, pump impeller blades and the like, that are required to produce hydrodynamic lift or thrust in a liquid by displacing the liquid through a movement of the article that creates lower pressure in the liquid on one side of the article and higher pressure on the other side.

More explicitly, the liquid is essentially displaced by both sides, being pressed into a new position on the high-pressure side and sucked it into a new position on the low pressure side by the movement of the article. The force needed to accelerate the mass of the liquid in the process of displacing it, is what provides the required hydrodynamic lifting or thrusting force on the article in the opposite direction.

However, the low pressure sides of such articles are prone to at least two phenomena that can suddenly and dramatically reduce the hydrodynamic lifting or thrusting ability of these articles as the speed of the movement is increased:

• 1. Firstly, the low pressure side can develop “cavitation”, which is the phenomenon of the liquid turning to gas, or boiling, due to substantially reduced pressure, caused by the liquid's inability to accelerate fast enough to occupy the space behind the passing article (also referred to as “inertial cavitation”). The boiling of the liquid consumes a large amount of energy that is released when the bubbles of gas collapse, producing tiny points of intense heat (hot enough to melt steel), substantially impairing the materials of the articles they contact. It must be noted that this energy is sacrificial since it does not enhance the lifting properties of the article, and therefor produces drag. Furthermore, the bubbles disturb the displacement of the liquid on the low pressure side of the article and dramatically reduce the hydrodynamic lifting or thrusting force of the article.
• 2. Secondly, a further drawback in using such articles at or near the surface is the “surface venting” of the article. This is the phenomenon that occurs when the surface air is sucked down into the low pressure side of the article, also disturbing the displacement of the liquid on the low pressure side and dramatically reducing the hydrodynamic lifting or thrusting force of the article.

SUMARY

An improved method or apparatus for creating required hydrodynamic lift or thrust in a liquid at high speed with a blade or blades comprising a wetted planing surface and a dry surface is presented. Each blade essentially contains only a high pressure surface in contact with the liquid, the low pressure surface being covered with an introduced gas, such as surface air, providing a blade that is essentially a single hydroplaning surface, below the liquid surface, planing in it's own “bubble” or gas filled void in the liquid. This completely eradicates the sudden loss of hydrodynamic lift and drag caused by cavitation. It also eradicates the sudden loss of lift at high speed caused by surface venting, since the blade or blades vent at low speeds and are already fully vented by the time they reach high speed. The blade can be set to a higher angle of attack to compensate for the loss of lift or thrust due to the low pressure surface not sucking down the liquid directly.

One possible embodiment of this invention is presented as a system or method of allowing high-speed aircraft to take off from, and alight on water using a retractable blade or blades.

Such an aircraft would be able to float on water by displacing the water with wings or fuselage, and as forward speed increases, the deployed blade, or blades present submerged surfaces that, with enough forward speed, “plane” under water, deriving the required hydrodynamic lift from the high pressure surface alone.

This embodiment intentionally allows the surface air to be sucked down and delaminate the flow of water on the low pressure surface, with the high pressure surface having sufficient angle of attack to provide enough hydrodynamic lift to support and raise the aircraft to sufficient altitude above the surface, that the correct angle of attack and speed on the main flying wing of the aircraft may be achieved to produce flight. Once airborne, the blade or blades can be retracted into the aircraft and will not present parasitic drag that can effect the aircraft's speed in flight.

While alighting on the water, the deployed blade or blades penetrate the surface as the aircraft descends, drawing down the air below the surface. The blades are immediately vented and thus impervious to cavitation, even at high speeds, while the angle of attack on the high pressure surface provides enough lift to support the aircraft.

By using blades tapered toward the tip, the minimum amount of surface is wetted to provide required hydrodynamic lift, allowing a decrease in drag from wetted surface as speed is increased and the blades rise out of the water.

A deflector flange may also be used at the leading edge on the low pressure side to encourage introduction of gas at low speed or at a low angle of attack.

To assist in lifting or thrusting at low speeds, an embodiment may have part of the blade or blades shaped as a hydrofoil, and the angle of attack may be variable.

With any embodiment, the blade or blades may be flexible to account for an uneven surface of the liquid, such as waves or swell.

Another embodiment of this invention is presented where this type of blade allows high-speed watercraft to exceed the speed where cavitation is reached.

A further embodiment is a method of introducing a gas, such as exhaust gas or surface air, to the front or low pressure surface of a boat propeller, reducing or totally eliminating cavitation and the sudden loss of thrust incidental to surface venting.

DRAWINGS

FIGS. 01-04 show planar view illustrations of various embodiments of blades in accordance with the invention.

FIGS. 05-07 show a typical cross section illustrations at “A” of the typical embodiments shown in FIGS. 01 through 04.

FIGS. 08-14 show possible front end elevation illustrations of possible embodiments of this invention where the blades lift an aircraft or vessel out of the water.

FIGS. 15-17 show possible planar, front end elevations and cross section view illustrations of an embodiment which is a combination of this invention and a conventional hydrofoil.

FIGS. 18-19 show possible perspective view illustrations of embodiments which are boat propellers.

FIGS. 20-22 show possible cross section illustrations of embodiments that can operate as a hydrofoil at low speeds and as a high speed blade in accordance with the invention.

FIGS. 23-24 show possible side view illustrations of the embodiment in FIGS. 20-22 that is inverted and attached to a pylon or boat rudder.

FIGS. 25-26 show possible top view illustrations of an embodiment as a pylon or boat rudder, traveling at both low speed and high speed respectively.

FIGS. 27-28 show possible top view illustrations of an embodiment as a pylon or boat rudder, traveling at both low speed and high speed respectively with deflection of liquid to one side.

REFERENCE NUMERALS

• 101 blade
• 102 leading edge
• 103 trailing edge
• 104 base
• 105 tip
• 106 liquid
• 107 general direction of blade movement through liquid
• 108 general direction of liquid acceleration due to blade movement
• 109 general direction of thrust
• 110 angle of attack
• 111 high pressure or planing surface of blade
• 112 low pressure or dry surface of blade
• 113 gas
• 114 void in liquid surrounding gas and blade
• 115 flange
• 116 increased thickness
• 117 object such as aircraft, boat or propeller hub
• 118 chine
• 119 gas passage
• 120 bend

DETAILED DESCRIPTION

As required, detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention that may be embodied in various and alternative forms. Specific structural and functional details, and shapes disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention.

Description—FIGS. 01 through 04

Some examples of the many such possible embodiments are shown in FIGS. 01 through 04 where planar views of the embodiments show blade 101 with leading edge 102 and trailing edge 103, and base 104 and tip 105, moving in direction 107.

Operation—FIGS. 01 through 04

To operate such embodiments, blade 101 is moved through liquid 106 (not shown) as depicted by movement 107.

Description—FIG. 05

FIG. 05 shows a typical cross section at “A” of the typical embodiments shown in FIGS. 01 through 04, where blade 101 is submerged, or partially submerged, in liquid 106, showing typical directional movement 107 of blade 101 at angle of attack 110 relative to the high pressure or planing surface 111. Leading edge 102 may be xyresic or rounded. Not shown, void 114 may extend behind trailing edge 103 multiple times the width of blade 101.

Operation—FIG. 05

To operate this embodiment, blade 101 is moved through liquid 106 in general direction 107 with enough speed and angle of attack 110 such that sufficient liquid 106 is accelerated with planing surface 111 alone, in general direction 108, to generate required hydrodynamic thrust on blade 101 in generally the opposite direction 109.

Such movement 107 of blade 101 at angle of attack 110 also causes relatively low pressure in liquid 106 adjacent to low pressure side 112 and which draws in gas 113 to create void 114 in liquid 106 that surrounds gas 113 and blade 101. The pressure in gas 113 being high enough that cavitation cannot occur on low pressure side 112.

Since blade 101 becomes fully vented at relatively low speed, and required hydrodynamic thrust or lift is generated by planing surface 111 alone, such embodiments are not prone to sudden loss of required hydrodynamic thrust or lift due to surface venting.

Description—FIG. 06

FIG. 06 shows a similar embodiment as FIG. 05, with the addition of flange 115 at leading edge 102 on low pressure side 112.

Operation—FIG. 06

Operating this embodiment is similar to FIG. 05 with the added ability of flange 115 to induce low pressure on side 112 to draw in gas 113 at a lower angle of attack 110 and at lower speeds than the embodiment of FIG. 05.

Description—FIG. 07

FIG. 07 shows an embodiment with the addition of increased thickness 116 of blade 101.

Operation—FIG. 07

Operating this embodiment is similar to previous embodiments with the addition of structural strength provided by increased thickness 116, which also allows blade 101 to produce required hydrodynamic lift or thrust, at a speed below that which draws in gas 113 to create void 114, similar to the known ability of a conventional hydrofoil.

Description—FIGS. 08 through 11

FIGS. 08 through 11 show possible front end elevations of embodiments of this invention with object 117 attached to blade 101A and blade 101B which are piercing the surface of liquid 106, and with void 114 in liquid 106 surrounding gas 113 and blades 101. FIG. 08A shows possible embodiments with blade 101 angled at bend 120 to provide additional lateral stability. FIG. 9 shows blades 101 attached at tips 105 to form a “v” and FIG. 10 shows blades 101 attached at tips 105 to form a continuous arc.

Operation—FIGS. 08 through 11

To operate these embodiments, blades 101A and 101B are moved through liquid 106 creating a high pressure and a low pressure in liquid 106 such that gas 113 is drawn onto low pressure side 112 to create void 114 in liquid 106, with enough speed to plane on the high pressure or planing surface 111, whereby deflecting liquid 106 with enough force to provide hydrodynamic thrust on blade 101 to lift object 117 above liquid 106. As shown in FIG. 11, the dihedral in blades 101A and 101B provide stability about the roll axis as thrust 109A is greatly diminished and thrust 109B greatly increased when object 117 is tilted to one side.

Description—FIGS. 12 through 14

FIG. 12 shows a possible front-end elevation of embodiments of this invention with blade 101 being curved or flexible.

FIG. 13 shows a possible front-end elevation of embodiments of this invention with blades 101 being retracted into object 117.

FIG. 14 shows a possible front-end elevation of embodiments of this invention with blade 101 having chines.

Operation—FIGS. 12 through 14

Operation of embodiments shown from FIGS. 12 through 14 is similar to previous embodiments with FIG. 13 showing the retraction of blades 101 in the case of object 117 being a high speed aircraft such as a jet.

Description—FIGS. 15 through 17

FIGS. 15 through 17 shows a type of embodiment which is a combination of this invention and a conventional hydrofoil, where part of blade 101 has a cross section similar to a conventional hydrofoil at B, and sections C through F show a progression of the transition to a single high speed wetted surface as shown in this invention.

Operation—FIGS. 15 through 17

Because a conventional hydrofoil known in the art has better lifting properties at low speed, a combination is presented whereby the upper portion of blade 101 can give more lift at low speeds and the lower portion of blade 101 will become fully vented and operate in accordance with the operation of FIGS. 05 through 07 at high speeds.

Description—FIGS. 18 through 19

FIGS. 18 through 19 show an embodiment of this invention where blade 101 is the blade of a propeller, and gas 113 can be exhaust gas or surface air that passes through gas passage 119 to create void 114 (not shown) in liquid 106 (not shown). FIG. 18 has the addition of flange 115.

Operation—FIGS. 18 through 19

Operation of these embodiments is similar to previous embodiments, where blade 101 is moved through liquid 106 (not shown) creating a high pressure and a low pressure in liquid 106 (not shown) such that gas 113 and is drawn through gas passage 119 onto low pressure side 112, to create void 114 (not shown) in liquid 106 (not shown), whereby allowing blade 101 to exceed the speed where cavitation is typical and also operate near or at the liquid surface without creating sudden loss of thrust due to surface venting.

Description—FIGS. 20 through 22

FIGS. 20 and 21 show an embodiment which is another combination of this invention and a conventional hydrofoil, where blade 101 has increased thickness 116 such that the after part of blade 101 has a cross section typical of a conventional hydrofoil.

FIG. 22 shows blade 101 with surface 111 as concave. Not shown, surface 111 may be convex or a combination of both concave and convex,

Operation—FIGS. 20 through 22

Because a conventional hydrofoil known in the art may have better lifting properties at low speed, a combination is presented to provide hydrodynamic lift when blade 101 is traveling in direction 107 at low speed as in FIG. 20. A small amount of gas 113 may be drawn in behind flange 115 to complete the hydrofoil shape. This space may also be filled with an eddy of liquid 106.

FIG. 21 shows the same embodiment as FIG. 20 with blade 101 traveling in direction 107 at high speed and providing required hydrodynamic lift in accordance with this invention.

Description—FIGS. 23 through 24

FIGS. 23 and 24 show an embodiment of this invention where blade 101 is attached perpendicularly to another blade 101A, such that it may be inverted to provide a downward thrust. Blade 101A may have gas passage 119 to supply gas 113 to low pressure side 112.

Operation—FIGS. 23 through 24

This embodiment is operated much the same as in FIGS. 20 and 21, but providing down thrust at both low speed and high speed, gas 113 being drawn in through gas passage 119.

Description—FIGS. 25 and 26

FIGS. 25 and 26 show an embodiment of this invention where blade 101 is symmetrical about the forward and aft axis, both sides being similar to low pressure surface 112 with flange 115. When used vertically as a ruder or pylon as with blade 101A in FIGS. 23 and 24, gas 113 may be drawn in through gas passage 119.

Operation—FIGS. 25 through 26

This embodiment may be operated at both high speed and low speed, with neutral thrust in either direction, with gas 113 being draw in to prevent cavitation on either side.

Description—FIGS. 27 and 28

FIGS. 27 and 28 show the same embodiment as FIGS. 25 and 26 where blade 101 can be angled to provide thrust to one side or the other as in the case of a rudder or center board.

Operation—FIGS. 27 through 28

This embodiment may be operated to provide thrust to one side or the other at both high speed and low speed, with gas 113 being draw in to prevent cavitation on either side.

Claims

1. An apparatus providing thrust to an object in a liquid comprising:

(a) least one blade that can move through said liquid with a leading edge and a trailing edge, a base and a tip, and with material in between that form a surface or surfaces on each side of said blade,

(b) means for attaching said blade or blades to said object,

(c) means for moving said object relative to said liquid,

(d) means for providing a gas to at least one side of said blade or blades, such that said blade or blades can be moved by said object through and separate said liquid with enough speed and angle of attack to generate a high pressure in said liquid on one side of said blade or blades and a low pressure in said liquid on said other side of said blade or blades, whereby said blade or blades can displace or accelerate enough liquid with said high pressure side to create required hydrodynamic thrust on said blade or blades in generally a perpendicular angle to the direction of said movement of said blade or blades, and, furthermore, said low pressure can draw in said gas to form a void in said liquid contiguous to said low pressure side, said void being able to extend behind said trailing edge in said liquid, whereby said liquid has substantially reduced contact with said low pressure side, and said blade can travel through said liquid with substantially reduced parasitic drag from wetted surface area, and whereby said blade is not subjected to sudden loss of hydrodynamic thrust due to cavitation as speed through said liquid is increased, and whereby said blade is not subjected to sudden loss of lift due to rapid surface venting as speed through said liquid is increased.

2. A blade as in claim 1 comprising added thickness in said material to provide addition strength to said blade.

3. A blade as in claim 1 with the addition of a flange at said leading edge on said low pressure side, said flange inducing said low pressure to draw in said gas and create said void at lower angles of attack and at lower speeds.

4. A blade as in claim 1 that is tapered toward said tip.

5. A blade or blades as in claim 1 where said object is an airplane or a vessel and said thrust of said blade or blades lifts part or all of said object above the surface of said liquid.

6. Blades as in claim 5 where said blades are set up as one or more laterally opposing pairs where said blades are angled toward one another at said tips in such a way that their combined thrust can lift said object and provide roll axis stability through dihedral.

7. A blade as in claim 1 where said liquid has a surface and above said liquid surface is air, said movement being more or less on the same plane as said liquid surface, and

furthermore, part of said blade is below said liquid surface and part of said blade is above said liquid surface,

whereby said air is drawn directly from above said liquid surface by said low pressure to form said void in said liquid contiguous to said low pressure side of said blade, thus venting said blade gradually as speed increases, and whereby said blade is not subjected to sudden loss of lift due to rapid surface venting or to cavitation as speed through said liquid is increased.

8. Blades as in claim 6 where said blades are joined at said tips to form a “v” shape.

9. Blades as in claim 6 where said blades are joined at said tips to form an arc.

10. A blade as in claim 1 that is partially shaped as a hydrofoil.

11. A blade as in claim 1 where said object is a hub of a propeller or a turbine.

12. A blade or blades as in claim 5 where said blade is retractable into said object.

13. A blade or blades as in claim 5 where said blade is not retractable into said object and provides aerodynamic lift to said object during flight.

14. A blade as in claim 1 where said gas is introduced to said low pressure side under pressure or by being pumped.

15. A blade as in claim 1 where said tip is bent in any direction to provide additional lateral stability.

16. A blade as in claim 1 where said angle of attack of said blade is adjustable.

17. A method providing thrust to an object in a liquid comprising:

(a) providing least one blade that can move through said liquid with a leading edge and a trailing edge, a base and a tip, and with material in between that form a surface or surfaces on each side of said blade,

(b) providing means for attaching said blade or blades to said object,

(c) providing means for moving said object relative to said liquid,

(d) providing means for providing a gas to at least one side of said blade or blades, such that said blade or blades can be moved by said object through and separate said liquid with enough speed and angle of attack to generate a high pressure in said liquid on one side of said blade or blades and a low pressure in said liquid on said other side of said blade or blades, whereby said high pressure provides thrust on said blade or blades in generally a perpendicular angle to the direction of said movement of said blade or blades, and furthermore, said low pressure can draw in said gas to form a void in said liquid contiguous to said low pressure side, said void being able to extend behind said trailing edge in said liquid, whereby said blade can displace enough liquid with said high pressure side alone to create required hydrodynamic thrust, and whereby said liquid has substantially reduced contact with said low pressure side, and said blade can travel through said liquid with substantially reduced parasitic drag from wetted surface area, and whereby said blade is not subjected to sudden loss of hydrodynamic thrust due to inertial cavitation as speed through said liquid is increased.